145436 ⎘
Geometry; Two-dimensional machined; miscellaneous bevelled
Rotor and turbo machine including same
#2Turbine blade having gas film cooling structure with a composite irregular groove and a method of manufacturing the same
#3Gas turbine blade for re-using cooling air and turbomachine assembly and gas turbine comprising the same
#4SELF-CENTERING SEAL AND METHOD OF USING SAME
#5Mate face arrangement for gas turbine engine components
#6Turbine rotor blade assembly
#7Method for modifying a shroud and blade
#8Gas turbine engine having a heat shield
#9Guide vane plate with a chamfered and a cylindrical edge region
#10Slide device, mechanical seal, pump and auxiliary artificial heart system
#11Heat shield for mixed flow turbine wheel turbochargers
#12Turbine blade or vane having a stepped and beveled platform edge
#13Gas turbine engine airfoil platform edge geometry
#14Rotor assembly for gas turbine
#15ATR axial V-groove
#16Integrated nozzle and plug
#17ATR full ring sliding nacelle
#18ATR guide pins for sliding nacelle
#19Tapered-land thrust bearing for turbochargers
#20Exhaust-gas turbocharger
#21Turbo-machinery rotors with rounded tip edge
#22Exhaust-gas turbocharger with silencer
#23Augmentor spray bar with tip support bushing
#24Turbine engine compressor stator
#25Gas turbine engine sealing structure
#26Chamfer-fillet gap for thermal management
#27System and method for cooling a wall of a gas turbine combustor
#28Chamfer rail pockets for turbine vane shrouds
#29TURBINE BLADE FOR A GAS TURBINE ENGINE
#30COMPONENT WITH DIAGONALLY EXTENDING RECESSES IN THE SURFACE AND PROCESS FOR OPERATING A TURBINE
#31Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws
#32Variable geometry turbine
#33Apparatus and method for reduction of jet noise from single jets
#34Shroud configuration having sloped seal
#35Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages
#36Bore and shaft assembly
#37Bore and shaft assembly
#38Bore and shaft assembly
#39Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows
#40Apparatus and method for reduction jet noise from single jets
#41Cantilevered stator stage